Cooperative Guidance Law with Impact Angle and Impact Time Constraints for Networked Missiles

doi:10.3969/j.issn.1000-1093.2016.03.007

Abstract

Abstract: Cooperative biased proportional guidance law with impact angle and impact time constraints is presented for cooperative attack of networked missiles. The biased proportional guidance law with impact angle constraints is proposed, and the expression of time-to-go in this guidance law is deduced. The proportional coefficient is adjusted by the difference of the time-to-go of each missile in the network. And the cooperative biased proportional guidance law with impact angle and impact time constraints is presented. It is proved theoretically that the multiple missiles trend to have the same time-to-go by the guidance law. Finally, the mathematical simulation of guidance system of networked missiles illustrates the validity of the proposed guidance law and the expression of time-to-go.

Key words: control science and technology, cooperative guidance law, impact angle constraint, impact time constraint, time-to-go

CLC Number:

TJ765.3

ZHANG Chun-yan, SONG Jian-mei, HOU Bo, ZHANG Min-qiang. Cooperative Guidance Law with Impact Angle and Impact Time Constraints for Networked Missiles[J]. Acta Armamentarii, 2016, 37(3): 431-438.

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